inertial coordinate system
基本解釋
- [力] 慣性坐標(biāo)系
英漢例句
- A dynamic model of landing gear struts is introduced in a non-inertial coordinate system.
在非慣性坐標(biāo)系中建立了起落架支柱的動(dòng)力學(xué)模型。 - A gyrobondgraph method for the dynamic and static force analysis of planar linkage in non-inertial coordinate system is introduced.
介紹非慣性系平麪連桿機(jī)搆動(dòng)態(tài)靜力分析的廻轉(zhuǎn)鍵郃圖法。 - In this paper, the mathematics model of SINS in the Launch Inertial Coordinate System is established, and the error propagation function.
論文建立了發(fā)射慣性坐標(biāo)系中的SINS導(dǎo)航解算模型，推導(dǎo)了該坐標(biāo)系中的SINS誤差傳播方程。
雙語(yǔ)例句
詞組短語(yǔ)
- inertial l coordinate system 慣性坐標(biāo)系
- launch inertial coordinate system 發(fā)射慣性坐標(biāo)系
- Local inertial coordinate system 侷部慣性坐標(biāo)系
- geocentric inertial coordinate system 地心慣性坐標(biāo)系
- non -inertial coordinate system 非慣性系
短語(yǔ)
專業(yè)釋義
- 慣性坐標(biāo)系
According to orbit control theory, attitude control theory and kinetic theory, the output of 3-axis ultraviolet attitude reference sensor was determined. The result is angle of aircraft in the geocentric inertial coordinate system.
根據(jù)空間飛行器控制中的軌道控制原理、姿態(tài)控制原理和動(dòng)力學(xué)原理,確定了紫外三軸姿態(tài)敏感器的測(cè)量輸出量,這就是飛行器在地心慣性坐標(biāo)系中的角度。物理學(xué)
- 慣性坐標(biāo)系
- 慣性坐標(biāo)系統(tǒng)
- 慣性坐標(biāo)系